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1. 发明申请

US20180045497A1 SYSTEM FOR VISUAL OBSCURATION OF AN OBJECT AND DISSIPATING ENERGY OF A LASER WEAPON 审中-公开
公开(公告)号：US20180045497A1
公开(公告)日：2018-02-15
申请号：US15234459
申请日：2016-08-11
申请人： The Boeing Company
发明人： Mark J. Clemen, JR. , Donald V. Drouin, JR. , Stephen N. Provost , Roger D. Bernhardt
IPC分类号： F42B12/48 , F41H13/00 , G01S17/02
CPC分类号： F42B12/48 , F41H3/02 , F41H5/007 , F41H9/06 , F41H13/005 , F41H13/0056 , F41H13/0062 , F41H13/0087 , G01S17/026
摘要： A visual obscurant system for obscuring object from an observer having a field of view (FOV) is disclosed. The system comprises a sensor for detecting characteristics that indicate a presence of the object, a light source for emitting light in an electromagnetic spectrum, a source, and a controller. The source releases an obscurant into atmosphere to create a cloud. The obscurant attenuates a portion of the electromagnetic spectrum. The cloud is positioned within the FOV of the observer so as to obscure the object when the light emitted from the light source is directed towards the cloud. The controller is in communication with at least the sensor and the source. The controller modulates the light source at a frequency sufficient such that the observer interprets the light as being constant when energized.

2. 发明申请

US20200269708A1 STRUCTURALLY INTEGRATED ENERGY SUPPLY SYSTEMS FOR AIRCRAFT AND METHODS OF FORMING THE STRUCTURALLY INTEGRATED ENERGY SUPPLY SYSTEMS 审中-公开
公开(公告)号：US20200269708A1
公开(公告)日：2020-08-27
申请号：US16282096
申请日：2019-02-21
申请人： The Boeing Company
发明人： Roger D. Bernhardt , Donald V. Drouin, JR.
IPC分类号： B60L50/60 , B64C3/18 , B64C1/12 , B64C3/20 , H01M2/10 , H01M10/0525
摘要： Structurally integrated energy supply systems for aircraft and methods of forming the structurally integrated energy supply systems. The structurally integrated energy supply systems include an aircraft structural component, a cell array, and a plurality of energy-producing inserts. The aircraft structural component at least partially defines an interior region. The cell array includes a plurality of cell walls that defies a plurality of elongate cell volumes and is positioned within the interior region. Each energy-producing insert in the plurality of energy-producing inserts is positioned within a corresponding elongate cell volume in the plurality of elongate cell volumes and is configured to produce a corresponding insert electric current. The cell array provides structural load distribution to the aircraft structural component via the plurality of cell walls and contributes to a structural stiffness of the aircraft structural component.

3. 发明申请

US20180105257A1 Inflatable Propeller 审中-公开
公开(公告)号：US20180105257A1
公开(公告)日：2018-04-19
申请号：US15292812
申请日：2016-10-13
申请人： The Boeing Company
发明人： Roger David Bernhardt , Donald V. Drouin, JR.
IPC分类号： B64C11/18 , B64C11/20 , B64B1/30 , B64C39/10
摘要： A method and apparatus for controlling movement of an aircraft. An aerodynamic function desired for controlling the movement of the aircraft at a particular altitude is identified. The aerodynamic function identified is part of a group of aerodynamic functions used to control the movement of the aircraft at a number of different altitudes. A group of inflatable blades is filled with a fluid to a pressure that corresponds to the aerodynamic function. The group of inflatable blades at the pressure has a shape and a group of dimensions that provide the aerodynamic function.

4. 发明申请

US20170284780A1 PROJECTILE DELIVERY OF DISRUPTIVE MEDIA FOR TARGET PROTECTION FROM DIRECTED ENERGY 有权
公开(公告)号：US20170284780A1
公开(公告)日：2017-10-05
申请号：US15088286
申请日：2016-04-01
申请人： The Boeing Company
发明人： Mark J. Clemen, JR. , Donald V. Drouin, JR.
IPC分类号： F42B12/50 , F42B12/48 , F41H13/00 , F42B15/01
CPC分类号： F42B12/50 , F41H13/0062 , F42B12/48 , F42B12/70 , F42B15/01 , F42C13/02
摘要： Methods, devices, and systems may protect a target from undesirable electromagnetic radiation by detecting electromagnetic radiation (including coherent radiation such as laser beams) aimed at a target from a source; calculating a first release position to disrupt the electromagnetic radiation thereby protecting the target; launching a projectile that may include a disruptive medium or a disruptive-medium precursor; directing the projectile to the first release position; and releasing the disruptive medium from the projectile at the first release position, such that the releasing of the disruptive medium forms a cloud of the disruptive medium.

5. 发明申请

US20170113785A1 SYSTEMS AND METHODS FOR PROTECTING A VEHICLE FROM A DIRECTED ENERGY ATTACK 有权
公开(公告)号：US20170113785A1
公开(公告)日：2017-04-27
申请号：US14923677
申请日：2015-10-27
申请人： The Boeing Company
发明人： Donald V. Drouin, JR. , Mark J. Clemen, JR.
IPC分类号： B64C13/16 , G05D1/10
CPC分类号： B64C13/16 , B64C19/00 , B64D45/0015 , B64D2045/0055 , F41H11/02 , F41H13/00 , G05D1/101 , Y02T50/44
摘要： A computer-implemented method for protecting a vehicle from a directed energy attack is provided. The method includes receiving, at the vehicle, a beam of directed energy, determining a threat level of the beam of directed energy, and causing the vehicle to automatically execute at least one evasive maneuver when the threat level of the beam of directed energy is greater than a predetermined threshold.

6. 发明申请

US20170248811A1 Window Method and Apparatus for Protection from Bright Light Sources 有权
公开(公告)号：US20170248811A1
公开(公告)日：2017-08-31
申请号：US15056415
申请日：2016-02-29
申请人： The Boeing Company
发明人： Mark J. Clemen, JR. , John R. Hull , Philip E. Johnson , Rick L. McGann , George A. Perry , Alan F. Stewart , Mark S. Wilenski , Donald V. Drouin, JR. , Le Li , Yongxin Tang , Haiping Yu , Jiangbin Zhao , Jie Yang , Shenggang Wang
IPC分类号： G02F1/1347 , B64C1/14 , B64D45/00 , G02F1/13363
CPC分类号： G02F1/1347 , B64C1/1484 , B64D45/00 , G02F1/13363 , G02F2001/133638 , G02F2001/13478 , G02F2203/05 , G02F2203/07 , G02F2203/09
摘要： According to an embodiment, an electrically switchable mirror includes: a first electrically switchable layer of cholesteric liquid crystal material, the first electrically switchable layer having a first state in which right-handed circularly polarized light incident thereon is reflected and left-handed circularly polarized light incident thereon is transmitted and a second state wherein right-handed and left-handed circularly polarized light incident thereon are transmitted; a second electrically switchable layer of cholesteric liquid crystal material, the second electrically switchable layer having a first state in which left-handed circularly polarized light incident thereon is reflected and right-handed circularly polarized light incident thereon is transmitted and a second state wherein right-handed and left-handed circularly polarized light incident thereon are transmitted; and a first electrically switchable wave plate disposed between the first and second electrically switchable layers.

7. 发明申请

US20170237947A1 DETECTING AND LOCATING BRIGHT LIGHT SOURCES FROM MOVING AIRCRAFT 审中-公开
公开(公告)号：US20170237947A1
公开(公告)日：2017-08-17
申请号：US15046224
申请日：2016-02-17
申请人： THE BOEING COMPANY
发明人： Mark J. Clemen, JR. , Donald V. Drouin, JR. , James A. Grossnickle
IPC分类号： H04N7/18 , H04N5/247 , B64D47/08 , G06T7/00
CPC分类号： H04N7/185 , B64D47/08 , G06T7/579 , G06T7/70 , G06T2207/30212 , G06T2207/30252 , H04N5/2254 , H04N5/2258 , H04N5/23206 , H04N5/247
摘要： A method and system for a light source detection system, comprising an aircraft carrying at least one camera. The system includes a database for storing information about the aircraft's motion, direction, and position and ground location information, such as the onboard navigation system database or an remotely accessible database. The system also includes a processor that accesses the database and is connected to the camera. The processor uses image analysis and processing techniques to determine the ground location corresponding to the light source from an image of that light captured by the camera. It determines the path traveled by that light and estimates its location as being a pre-selected distance vertically above the ground along the path traveled by the light to the aircraft when the image of the light was captured.

8. 发明申请

US20170129592A1 Mitigating Shock Using Plasma 有权
公开(公告)号：US20170129592A1
公开(公告)日：2017-05-11
申请号：US14936953
申请日：2015-11-10
申请人： The Boeing Company
发明人： Mark Joseph Clemen, JR. , Donald V. Drouin, JR. , Alan F. Stewart
IPC分类号： B64C21/00 , B64C23/00
CPC分类号： B64C21/00 , B64C23/00 , B64C23/005 , B64C30/00 , B64C2230/12
摘要： A method, apparatus, and system for mitigating undesired effects of a vehicle traveling at a speed greater than a critical Mach number for the vehicle. Ultraviolet energy is generated using a plurality of ultraviolet energy sources associated with an interior structure of the vehicle that travels at the speed greater than the critical Mach number for the vehicle. The ultraviolet energy is transported from the plurality of ultraviolet energy sources past an exterior of the vehicle around a selected location of the vehicle. A plasma is created around the selected location to mitigate the undesired effects of the vehicle traveling at the speed greater than the critical Mach number for the vehicle.

9. 发明申请

US20150274280A1 AIR VEHICLE, ACTUATOR ASSEMBLY AND ASSOCIATED METHOD OF MANUFACTURE 有权
标题翻译：空中车辆，执行机构总成及相关制造方法
公开(公告)号：US20150274280A1
公开(公告)日：2015-10-01
申请号：US14242088
申请日：2014-04-01
申请人： The Boeing Company
发明人： James Joseph Sheahan, JR. , Donald V. Drouin, JR.
IPC分类号： B64C13/34 , B64C13/26 , B64C9/00
CPC分类号： B64C13/34 , B64C9/00 , B64C9/02 , B64C13/26 , B64C13/38 , B64C13/40 , B64C13/50 , Y02T50/32 , Y02T50/44 , Y10T29/49826
摘要： An air vehicle, an actuator assembly and a method of manufacture are provided in order to incorporate the actuator assembly within the outer mold line of the air vehicle. In regards to an air vehicle, the air vehicle includes a primary structure and a movable structure configured to be controllably moved relative to the primary structure. The air vehicle also includes an actuator assembly configured to cause the movable structure to be positioned relative to the primary structure. The actuator assembly includes an actuator housing and an actuation mechanism. The actuation mechanism is at least partially disposed within the actuator housing and is configured to provide for relative movement between the primary structure and the movable structure. At least a portion of the actuator assembly is built into at least one of the primary structure and the movable structure so as to be within an outer mold line of the air vehicle.
摘要翻译：提供了一种机动车辆，致动器组件和制造方法，以将致动器组件并入到空中交通工具的外部模具线内。关于空中交通工具，该空中交通工具包括主结构和可相对于主结构可控制地移动的可移动结构。空中车辆还包括构造成使可移动结构相对于主结构定位的致动器组件。致动器组件包括致动器壳体和致动机构。所述致动机构至少部分地布置在所述致动器壳体内，并且构造成提供所述主结构和所述可移动结构之间的相对运动。致动器组件的至少一部分内置在主结构和可移动结构中的至少一个中，以便在空中车辆的外部模具线内。

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